Nose cone comprises the most significant component while designing high speed aircrafts. The objects moving at high
speeds encounter forces which tend to decelerate the objects. The resistance that is set up in the medium is known as drag and it
is concerned while designing high speed aircrafts. Nose cones of power series 0.6 and 0.75 are studied with respect to different
Mach numbers over a range 1 - 12 and analyzed using CFD analysis. The drag and stagnation properties of nose cones are
compared between them and with analytically calculated calculations. The aim of the paper is designing a hypersonic nose cone
with minimum air drag values and to predict those values.
